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dc.contributor.authorZhang, Zhipeng
dc.contributor.authorYuan, Qiangbo
dc.contributor.authorYin, Yin
dc.contributor.authorLiang, Taotao
dc.contributor.authorLiu, Lincheng
dc.date.accessioned2026-08-20T21:14:18Z
dc.date.available2026-08-20T21:14:18Z
dc.date.copyright2025/10/17
dc.date.issued2026
dc.identifier.otherJAEEEZ.ASENG-6418.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4314163
dc.description.abstractAbstractThe locking mechanism assumes the responsibility of locking the landing gear in the extended position, which is the key to ensure that the landing gear is stable to withstand the landing load of the aircraft. However, the reciprocating change in ...
dc.publisherAmerican Society of Civil Engineers
dc.titleSingularity Analysis and Optimization Design for Landing Gear Locking Performance Considering Ground Loads
dc.typeJournal Article
dc.journal.volume39
dc.journal.issue1
dc.journal.titleJournal of Aerospace Engineering
dc.identifier.doi10.1061/JAEEEZ.ASENG-6418
dc.journal.fristpage04025116-1
dc.journal.lastpage04025116-14
dc.page14
dc.treeJournal of Aerospace Engineering:;2026:;Volume ( 039 ):;issue: 001
dc.contenttypeFulltext


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